journal article·2007-06

Crack growth induced by sonic IR inspection

John C. Chen, Jacob Kephart, Kyle Lick, William T. Riddell

Publisher page

Abstract

We have developed an experiment to study the propagation of laboratory-synthesized fatigue cracks under various controlled conditions during Sonic IR inspection. The experiment provides for good repeatability in testing. The parameters of interest include the initial crack length, load history (stress intensity and load ratio) during crack generation, geometry of the crack, material and also the various conditions involving the ultrasonic excitation source. In general, we find that under typical sonic IR inspection conditions, the initial crack will propagate under sonic IR testing. The crack growth after each inspection event varies and exhibits a distribution in length of propagation. The results show that the average crack propagation decreases with increasing stress intensity factor, and we test two hypotheses about the cause of this. Furthermore, we find that crack propagation is affected by the initial crack length.
Source: openalex_inverted_index · Quality: baseline

Research context

OpenAlex topics: Thermography and Photoacoustic Techniques · Ultrasonics and Acoustic Wave Propagation · Structural Health Monitoring Techniques

SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.

References (10)

Show source-provided references
1. ASTM E647-00, Standard test method for measurement of fatigue crack growth rates, ASTM International 2005.
2. Chen J.C. · 2006 · 820 · 1577
3. 10.1063/1.115063010.1063/1.1150630 ↗
4. 10.1063/1.151624010.1063/1.1516240 ↗
5. 10.1063/1.165224310.1063/1.1652243 ↗
6. Levy, M., Assessment of damage tolerance requirements and analyses—tasks II and IV report, AFWAL-TR-86-3003, Vol. 4, Raw Test Data 1986.
7. 10.1016/0041-624X(81)90095-010.1016/0041-624X(81)90095-0 ↗
8. 10.1016/S0963-8695(97)00021-210.1016/S0963-8695(97)00021-2 ↗
9. Riddell, W.T. and Piascik, R.S., Stress ratio effects on crack opening loads and crack growth rates in aluminum alloy 2024, NASA Technical Memorandum TM-1998-206929, Langley Research Center 1998.10.1520/STP14961S ↗
10. Thomas, Infrared imaging of ultrasonically excited subsurface defects in materials, US Patent 6,236,049. May 22 et al., 2001.